Retaining tab for diffuser seal ring

Patent metadata

Field	Value
Publication number	US-2016348581-A1
Application number	US-201615165245-A
Country	US
Kind code	A1
Filing date	May 26, 2016
Priority date	May 29, 2015
Publication date	Dec 1, 2016
Grant date	—

Abstract

An example diffuser assembly includes a diffuser case, an annular ring, and a retaining tab that is mounted to the annular ring and has an end that engages an inner wall of the diffuser case. The engagement between the second end and the inner wall locks the retaining tab and limits movement of the annular ring along a central longitudinal axis of the diffuser case. Another example diffuser assembly includes a diffuser case, an annular ring, and a snap ring. The snap ring is situated in an annular groove of an inner wall of the diffuser case, and restricts movement of the annular ring along a central longitudinal axis of the diffuser case. A retaining tab is affixed to either the annular ring or the diffuser case, and has an end retaining the annular ring in the annular groove.

First claim

We claim:

1 . A diffuser assembly comprising:
a diffuser case; an annular ring; and a retaining tab that is mounted to the annular ring and has an end that engages an inner wall of the diffuser case, the engagement between the second end and the inner wall locking the retaining tab and limiting movement of the annular ring along a central longitudinal axis of the diffuser case.

2 . The diffuser assembly of claim 1 , wherein the end of the retaining tab is a second end that is part of a secondary portion of the retaining tab that extends radially outwards from the central longitudinal axis, and an opposite first end of the retaining tab is part of a primary portion of the retaining tab that is angled with respect to the secondary portion at an obtuse angle.

3 . The diffuser assembly of claim 2 , wherein an area of the primary portion is greater than an area of the secondary portion.

4 . The diffuser assembly of claim 1 , wherein the annular ring is configured as a seal within the diffuser case.

5 . The diffuser assembly of claim 1 , wherein the diffuser case defines an annular groove along its inner wall, and the end of the retaining tab is situated in the annular groove.

6 . The diffuser assembly of claim 5 , further comprising a snap ring situated in the annular groove, wherein the end of the retaining tab is situated between opposing ends of the snap ring.

7 . The diffuser assembly of claim 5 , further comprising a slot situated within the annular groove, the retaining tab comprising a tooth that engages an end wall within the slot, the engagement between the tooth and the end wall limiting rotation of the annular ring about the central longitudinal axis.

8 . The diffuser assembly of claim 1 , wherein the annular ring comprises an inner cylindrical section and an outer frustoconical section that is sloped with respect to the cylindrical section, and an inner diameter of the frustoconical section connects to the cylindrical section, and an outer diameter of the frustoconical section abuts the inner wall.

9 . The diffuser assembly of claim 8 , wherein each retaining tab is mounted to the annular ring via one or more fasteners, each fastener extending through an opening in the retaining tab that is aligned with an opening in the frustoconical section.

10 . The diffuser assembly of claim 9 , wherein the retaining tab is situated between a head of the fastener and an inner face of the frustoconical portion, and the annular ring provides an open band around the head of the fastener.

11 . The diffuser assembly of claim 10 , wherein the open band has a diameter that is at least three times larger than a diameter of the opening in the retaining tab.

12 . The diffuser assembly of claim 9 , wherein the end of the retaining tab is a second end that is opposite a first end, and the opening in the frustoconical section is closer to the first end of the retaining tab than to the second end of the retaining tab.

13 . A method comprising:
mounting a first end of a retaining tab to a frustoconical section of an annular ring that is sloped with respect to a cylindrical section of the annular ring, the annular ring being situated within a diffuser case of a gas turbine engine; and engaging an opposite second end of the retaining tab with an inner wall of the diffuser case, the engagement between the second end and the inner wall locking the retaining tab and limiting movement of the annular ring along a central longitudinal axis of the diffuser case.

14 . The method of claim 13 , wherein the diffuser case defines an annular groove along its inner wall, and the engaging comprises situating the second end of the retaining tab in the annular groove.

15 . The method of claim 14 , wherein the mounting and engaging are performed such that the annular ring is aft of the annular groove.

16 . A gas turbine engine comprising:
a high pressure compressor; a combustor that is in fluid communication with the high pressure compressor; a diffuser case situated between the high pressure compressor and combustor; an annular ring situated within the diffuser case; and a retaining tab having a first end that is mounted to the annular ring and an opposite second end that engages an inner wall of the diffuser case, the engagement between the second end and the inner wall locking the retaining tab and limiting movement of the annular ring along a central longitudinal axis of the gas turbine engine.

17 . A diffuser assembly comprising:
a diffuser case; an annular ring; a snap ring situated in an annular groove of an inner wall of the diffuser case, the snap ring restricting movement of the annular ring along a central longitudinal axis of the diffuser case; and a retaining tab that is affixed to either the annular ring or the diffuser case, and has an end retaining the annular ring in the annular groove.

18 . The diffuser assembly of claim 17 , wherein the end extends in a direction that is parallel to the central longitudinal axis.

19 . The diffuser assembly of claim 17 , wherein the end is a second end that is cantilevered and is opposite of a first end, and wherein the retaining tab is affixed to the annular ring or the diffuser case at the first end.

20 . The diffuser assembly of claim 19 , wherein the second end abuts the snap ring.

21 . The diffuser assembly of claim 19 , wherein a radial distance between the second end and an inner diameter of the snap ring is less than a radial distance between an outer diameter of the snap ring and the inner wall.

Assignees

• United Technologies Corp

Inventors

• Wiedemer John D
• Petty Dale William
• Lemoine Jonathan
• Arnold Jason

Classifications

• F01D11/12

  using a rubstrip, e.g. erodible. deformable or resiliently-biased part · CPC title

• F01D11/02

  by non-contact sealings, e.g. of labyrinth type (for sealing space between rotor blade tips and stator F01D11/08) · CPC title

• F05D2220/323

  for aircraft propulsion, e.g. jet engines · CPC title

• F05D2240/55

  Seals · CPC title

• F02C7/04 Primary

  Air intakes for gas-turbine plants or jet-propulsion plants · CPC title